References
CHAPTER 1
[1] Aeronautical Radio, Inc. ARINC Characteristics and Specifications for Navigation Equipment. Airlines Electronic Engineering Committee. Annapolis, MD.
[2] Cohen. C. E., et al. Real-time flight testing using integrity beacons for GPS Category III precision landing. Navigation 41:2 (1994): 145–157, Institute of Navigation, Alexandria, VA.
[3] International Civil Aviation Organization. Reports of the Future Air Navigation System (FANS) Committee. Montreal, Canada.
[4] Kelly, R. J., and J. M. Davis. Required navigation performance for precision approach and landing with GNSS application. Navigation 41:1 (1994): 1–30, Institute of Navigation, Alexandria, VA.
[5] RTCA, Inc. Produces Minimum Aviation System Performance Specifications (MASPS) and Minimum Operational Performance Standards (MOPS) for airborne and ground avionics using DO-xxx report numbers. Washington, D.C.
(a) “Environmental Conditions and Test Procedures for Airborne Equipment,” DO-160D (1997).
(b) “Minimum Operational Performance Standards for Airborne Automatic Dependent Surveillance (ADS) Equipment,” DO-212, 1992.
[6] U.S. Departments of Transportation and Defense. Federal Radionavigation Plan. Published in even-numbered years. Washington, DC, 175 pp.
[7] U.S. Federal Aviation Administration. Advisory Circulars Especially the AC-20-xx and AC-90-xx series on navigation. Washington, DC.
[8] U.S. Federal Aviation Administration. Technical Standard Orders TSO-C91 (1985) and TSO C126 (1992). Emergency ...
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